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A Wind Tunnel Operation Control System Based on Distributed Architecture

A distributed architecture and operation control technology, applied in the general control system, control/regulation system, program control, etc., can solve the extremely demanding requirements for coordination and timing control, the inability to achieve timing control and coordination, and the lack of management mechanisms, etc. problem, to achieve accurate and reliable sequential action logic, reduce long-distance transmission, and improve reliability and accuracy

Active Publication Date: 2020-03-24
BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE +1
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

The gas flow supersonic wind tunnel system has many links, and the high-temperature and high-pressure test environment generated is extremely harsh. The coordination and timing control requirements of various components are extremely strict. A slight error may cause the equipment to burn out and affect the success of the test.
The traditional wind tunnel system lacks a unified management mechanism, and the functions of each component are relatively independent, which cannot achieve high-demand timing control and coordination

Method used

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  • A Wind Tunnel Operation Control System Based on Distributed Architecture
  • A Wind Tunnel Operation Control System Based on Distributed Architecture
  • A Wind Tunnel Operation Control System Based on Distributed Architecture

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Embodiment Construction

[0054] The composition of the wind tunnel operation control system based on the distributed architecture of the present invention is as follows: figure 1 As shown, it includes the general control command and dispatch subsystem, the gas main heater working condition adjustment subsystem, the gas main heater timing control subsystem, the spray condensation vacuum control subsystem, the main test bench control subsystem, and the normal temperature water supply control subsystem. Subsystem and air source supply control subsystem.

[0055] Working condition adjustment subsystem of the main gas heater: in the test preparation stage, it receives the dispatch instructions from the general control command and dispatch subsystem, completes the pipeline pressure adjustment of the main heater fuel circuit, oxygen circuit and high-pressure cooling water circuit, and sends to the general control command dispatch Subsystem feedback completion status.

[0056] The gas main heater working con...

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Abstract

The invention discloses a wind tunnel operation control system based on a distributed architecture, which belongs to the technical field of aerospace ground thermal insulation tests, so as to controleach part in a combustion-gas flow thermal wind tunnel test system to realize thermal examination on a spacecraft thermal protection structure. The distributed control architecture is used, each control subsystem of the wind tunnel has an independent controller, operation control is carried out on a corresponding device, coordination of the whole action is realized through a top-layer master control command and dispatch subsystem, the whole wind tunnel system is ensured to act in a coordinated and orderly mode, software and hardware supports are provided for stable operation of the wind tunnelsystem, and a technical support is provided for condition monitoring and timing control on the equipment.

Description

technical field [0001] The invention relates to a wind tunnel operation control system based on a distributed architecture, which is used to control various parts of the gas flow thermal wind tunnel test system to realize thermal assessment of spacecraft heat-resistant structural parts, and belongs to the technical field of aerospace ground heat-insulation tests . Background technique [0002] The gas flow test is a key link in the ground assessment of the heat protection system. It has the characteristics of high energy density, high total temperature, and harsh thermal environment. It is an irreplaceable test method for thermal assessment of heat protection materials and structures. However, the assessment of large-scale heat-resistant structural test pieces needs to be carried out on the basis of the gas flow supersonic wind tunnel, which is different from the conventional room temperature aerodynamic test wind tunnel. The expansion and acceleration of the nozzle generat...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M9/04G01M9/06G05B19/418G05D27/02
CPCG01M9/04G01M9/065G05B19/4183G05B2219/25232G05D27/02
Inventor 张凯齐斌宋文潇田宁邹样辉赵玲曹知红岳晖张利嵩那伟杨驰李彦良夏吝时张昕曹宇清姜一通李文浩鲁宇朱广生李建林孟刚周岩水涌涛张岩陈卫国黄凯王树信
Owner BEIJING AEROSPACE INST OF THE LONG MARCH VEHICLE
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